As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REMOVE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING STEP'S 1 THRU 8 RIGHT SIDE. REMOVED FLAP ACTUATOR AND INSTALLED IAW MM 27-52-01-2 AND ACCOMPLISHED EO 8-5720- 7-2302 STEP NR 1 THRU NR 8 RIGHT SIDE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING REPLACEMENT.